A nanowire magnetic sensor includes an array of magneto-resistive (mr) nanosensors with each mr nanosensor including a set of mr nanowires that are all aligned in the same position for one direction. The substrate can be a flexible substrate bent into a circular configuration for compass applications. A plurality of individual nanosensors can be connected into resistive Wheatstone bridge configurations by metallization.
|
9. A nanowire magnetic sensor, comprising:
a substrate;
a plurality of magneto-resistive (mr) nanowires on said substrate;
an array of mr nanosensors each comprising a set of said plurality of mr nanowires, wherein said mr nanowires in said sets are all aligned in the same position for one direction, and
metal lines for interconnecting said plurality of mr nanosensors in said array.
1. A method for fabricating a nanowire magnetic sensor, comprising:
forming a plurality of magneto-resistive (mr) nanowires on a flexible substrate, wherein said plurality of mr nanowires are positioned to create an array of mr nanosensors, and wherein each of said mr nanosensors in said array comprises a set of said plurality of mr nanowires,
wherein said mr nanowires in said sets are each aligned in the same position for one direction; and
connecting said array mr nanosensors into at least one Wheatstone bridge configuration.
2. The method of
3. The method of
4. The method of
5. The method of
6. The method of
7. The method of
8. The method of
10. The nanowire magnetic sensor of
11. The nanowire magnetic sensor of
12. The nanowire magnetic sensor of
13. The nanowire magnetic sensor of
14. The nanowire magnetic sensor of
15. The nanowire magnetic sensor of
16. The nanowire magnetic sensor of
17. The nanowire magnetic sensor of
|
This application is a continuation-in-part (CIP) of U.S. Non-provisional application Ser. No. 12/184,772 filed Aug. 1, 2008, which is herein incorporated by reference in its entirety.
Disclosed embodiments are generally related to magnetic sensors having a plurality of sensing elements.
Various types of equipment and systems for assisting in navigation and determining the location of a vehicle such as a boat, truck, automobile or airplane are known to the art. Such equipment and systems include various sensors for magnetic-effect sensing. Examples of common magnetic-effect sensors include Hall effect and magneto-resistive (MR) technologies. Such magnetic sensors can generally respond to a change in the magnetic field as influenced by the presence or absence of a ferromagnetic target object of a designed shape passing by the sensory field of the magnetic-effect sensor. The sensor can then provide an electrical output, which can be further modified as necessary by electronics to yield sensing and control information. The electronics may be located either onboard or outboard of the sensor package.
Various types of non-contact devices are presently available for measuring distance and detecting the linear or rotational position of an object. A magnetic compass is a navigational instrument for finding directions on the earth. A magnetic compass includes a magnetized pointer free to align itself accurately with earth's magnetic field, which is of great assistance in navigation. The face of the compass generally highlights the cardinal points of north, south, east and west. Magnetic position sensors utilized by the magnetic compass measure the direction and magnitude of magnetic fields by employing the MR effect. Such sensors include two galvanic separated Wheatstone bridges for sensing the position of a magnetic object. Such magnetic position sensors are generally non-contact sensors. As the magnetized pointer approaches the sensing device, the magnetic field of the pointer is detected and the sensing device generates an electrical signal that is then used for counting, display purposes, recording and/or control purposes.
Navigation generally requires a magnetic compass having an angular resolution of 0.01 to 0.001 degree or better for precise position determination, especially in a Global Positioning System (GPS) denied environment. Similarly, relative versus absolute azimuth resolution of the magnetic compass must also be high. Conventional magnetic position sensors provide a precision of about 0.1 degree, are expensive, and are limited to an accuracy of about 5.5 millidegrees (i.e., 16 bits).
This Summary is provided to comply with 37 C.F.R. §1.73, presenting a summary of the disclosed embodiments to briefly indicate the nature and substance disclosed herein. It is submitted with the understanding that it will not be used to interpret or limit the scope or meaning of the claims.
Nanowire magnetic compasses and position sensors for determining the position of a magnetic object or direction of a magnetic field are disclosed herein. Embodied as a magnetic compass, the magnetic compass includes an array of MR nanosensors on a flexible substrate, which cover the full 360-degree angle, in one embodiment at equal intervals. Each MR nanosensor generally includes MR nanowires with high magnetic sensitivity arranged in sets that are each aligned in the same position for one direction (e.g., aligned vertically), such as 2 to 50 MR nanowires aligned in the vertical direction on the substrate for each MR nanosensor. A plurality of nanosensors can be connected into resistive Wheatstone bridge configurations by metallization. In another embodiment, the array of MR nanosensors can be utilized as a position sensor for a magnetic object or an object having a magnet affixed thereon for position determination of the object.
Embodied as a compass, using a flexible substrate, the azimuth resolution and sensitivity of the compass can be increased by bending the flexible substrate to form a circular configuration. Each of the groups of MR nanowires for each of the MR nanosensor in the array will point at a different azimuth direction that is determined by the number of the nanosensors (e.g., 100 groups of nanosensors can cover 360 degrees in 3.6 degree intervals). Knowledge of that interval helps to increase precision of the magnetic compass. Additional electronics, such as preamplifiers, can also be provided on the substrate.
Individual nanosensors in the array can be connected into resistive bridge configuration. The MR nanowires can comprise Anisotropic Magneto-Resistive (AMR), Giant Magneto-resistive (GMR), colossal magnetoresistive, or tunneling magnetoresistive nanowires. By utilizing multiple nanosensors, the capability of extended angular or linear position measurements can be enhanced. The output of the resistive bridges can be aggregated in order to obtain high precision. For compass applications, a circular configuration can be formed with a diameter of 0.05 to 50 mm, such as on the order of 1 mm. Disclosed nanowire magnetic compasses and position sensors sensitive, low field, solid-state and able to measure direction and magnitude of earth's magnetic fields with high resolution
Disclosed embodiments are described with reference to the attached figures, wherein like reference numerals are used throughout the figures to designate similar or equivalent elements. The figures are not drawn to scale and they are provided merely to illustrate the disclosed embodiments. Several aspects are described below with reference to example applications for illustration. It should be understood that numerous specific details, relationships, and methods are set forth to provide a full understanding of the disclosed embodiments. One having ordinary skill in the relevant art, however, will readily recognize that the disclosed embodiments can be practiced without one or more of the specific details or with other methods. In other instances, well-known structures or operations are not shown in detail to avoid obscuring the disclosed embodiments. The disclosed embodiments are not limited by the illustrated ordering of acts or events, as some acts may occur in different orders and/or concurrently with other acts or events. Furthermore, not all illustrated acts or events are required to implement a methodology in accordance with disclosed embodiments.
As shown in
Embodied as a flexible substrate, the flexible substrate can be bent into a circular configuration apparatus for use as a compass for covering a 360-degree angle at equal intervals. For compass applications, the substrate 110 generally comprises a flexible substrate 110. The sets of MR nanowires 120 for each MR nanosensor 130 are shown in
The MR nanowires 120 can be printed and patterned on the flexible substrates 110 by photolithography or printing technique. Photolithography printing involves the deposition of a layer of photosensitive material on a semiconductor substrate, exposure of the photosensitive material through a mask, and development of the exposed photosensitive layer. Exposure is typically carried out in a scanner or stepper tool, wherein an exposure slit is passed across the surface of the substrate, thereby sequentially exposing narrow strips of the photosensitive layer. It can be appreciated that other types of printing techniques may also be utilized to print MR nanowires 120 on the flexible substrate 110, depending upon design considerations.
Since each MR nanosensor 130 shown in
Apparatus 100 can be utilized as a position sensor for determining the position of a magnetic object with the precision determined by the length of each MR nanosensor 130 shown as being in the x-direction in
The arrangement for achieving high sensitivity of the individual nanowires in the Wheatstone bridge is different for AMR with cos ^2 angle between nanowire axis (current direction) and magnetic field dependence and GMR with (1-cos (a))/2 dependence where ‘a’ is an angle between the nanowire axis and magnetic field. For example the AMR configuration may involve the nanosensors 320, 330, 340, and 310 of
The MR nanosensors 130 in nanowire sensor apparatus according to disclosed embodiments can be designed to accurately detect the direction and magnitude of external magnetic fields for compassing and magnetometry applications. Such sensor apparatus extremely sensitive, low field, solid-state magnetic sensors in one application able to measure the direction and magnitude of earth's magnetic fields. Similarly, the size of the array of nanosensors 130 and the small dimension of the MR nanowires 120 enables very high resolution forming low cost sensors for compassing and position determination.
While various embodiments have been described above, it should be understood that they have been presented by way of example only, and not limitation. Numerous changes to the disclosed embodiments can be made in accordance with the disclosure herein without departing from the spirit or scope of the disclosed embodiments. Thus, the breadth and scope of the disclosed embodiments should not be limited by any of the above explicitly described embodiments. Rather, the scope of the invention should be defined in accordance with the following claims and their equivalents.
Although the disclosed embodiments have been illustrated and described with respect to one or more implementations, equivalent alterations and modifications will occur to others skilled in the art upon the reading and understanding of this specification and the annexed drawings. In addition, while a particular feature may have been disclosed with respect to only one of several implementations, such feature may be combined with one or more other features of the other implementations as may be desired and advantageous for any given or particular application.
The terminology used herein is for the purpose of describing particular embodiments only and is not intended to be limiting to embodiments of the invention. As used herein, the singular forms “a,” “an,” and “the” are intended to include the plural forms as well, unless the context clearly indicates otherwise. Furthermore, to the extent that the terms “including,” “includes,” “having,” “has,” “with,” or variants thereof are used in either the detailed description and/or the claims, such terms are intended to be inclusive in a manner similar to the term “comprising.”
Unless otherwise defined, all terms (including technical and scientific terms) used herein have the same meaning as commonly understood by one of ordinary skill in the art to which the disclosed embodiments belong. It will be further understood that terms, such as those defined in commonly used dictionaries, should be interpreted as having a meaning that is consistent with their meaning in the context of the relevant art and will not be interpreted in an idealized or overly formal sense unless expressly so defined herein.
The Abstract of the Disclosure is provided to comply with 37 C.F.R. §1.72(b), requiring an abstract that will allow the reader to quickly ascertain the nature of the technical disclosure. It is submitted with the understanding that it will not be used to interpret or limit the scope or meaning of the following claims.
Patent | Priority | Assignee | Title |
10718636, | Apr 11 2012 | Louisiana Tech Research Corporation | Magneto-resistive sensors |
8441255, | Jan 22 2009 | Louisiana Tech Research Corporation | Thermocooling of GMR sensors |
8840271, | Jul 24 2012 | ABL IP Holding LLC | In-plane bent printed circuit boards |
9103654, | Apr 11 2012 | Louisiana Tech Research Corporation | GMR nanowire sensors |
9182459, | Sep 08 2011 | Honeywell International Inc.; Honeywell International Inc | Wireless magnetic position sensor |
9360345, | Oct 10 2011 | Honeywell International Inc.; Honeywell International Inc | Extended smart position sensing range using electromagnetics |
9784802, | Apr 11 2012 | Louisiana Tech Research Corporation | GMR nanowire sensors |
Patent | Priority | Assignee | Title |
5521501, | Jun 09 1993 | Sensitec GmbH | Magnetic field sensor constructed from a remagnetization line and one magnetoresistive resistor or a plurality of magnetoresistive resistors |
5714536, | Jan 11 1996 | Xerox Corporation | Magnetic nanocompass compositions and processes for making and using |
5889091, | Jan 11 1996 | Xerox Corporation | Magnetic nanocompass compositions and processes for making and using |
6373242, | Dec 09 1999 | Forskarpatent I Uppsala AB | GMR sensor with a varying number of GMR layers |
20070297102, | |||
20100024231, | |||
20100124091, | |||
JP2002310659, | |||
JP2004205331, | |||
JP2006010591, |
Executed on | Assignor | Assignee | Conveyance | Frame | Reel | Doc |
Dec 17 2009 | Honeywell International Inc. | (assignment on the face of the patent) | / | |||
Feb 18 2010 | PECZALSKI, ANDRZEJ | Honeywell International Inc | ASSIGNMENT OF ASSIGNORS INTEREST SEE DOCUMENT FOR DETAILS | 023972 | /0734 |
Date | Maintenance Fee Events |
Nov 28 2014 | REM: Maintenance Fee Reminder Mailed. |
Apr 19 2015 | EXP: Patent Expired for Failure to Pay Maintenance Fees. |
Date | Maintenance Schedule |
Apr 19 2014 | 4 years fee payment window open |
Oct 19 2014 | 6 months grace period start (w surcharge) |
Apr 19 2015 | patent expiry (for year 4) |
Apr 19 2017 | 2 years to revive unintentionally abandoned end. (for year 4) |
Apr 19 2018 | 8 years fee payment window open |
Oct 19 2018 | 6 months grace period start (w surcharge) |
Apr 19 2019 | patent expiry (for year 8) |
Apr 19 2021 | 2 years to revive unintentionally abandoned end. (for year 8) |
Apr 19 2022 | 12 years fee payment window open |
Oct 19 2022 | 6 months grace period start (w surcharge) |
Apr 19 2023 | patent expiry (for year 12) |
Apr 19 2025 | 2 years to revive unintentionally abandoned end. (for year 12) |